{"title":"基于Gps天线阵列的Gps/ins集成导航","authors":"K. J. Turner, F. Faruqi","doi":"10.1109/ISSPA.1996.615726","DOIUrl":null,"url":null,"abstract":"An integrated Global Positioning System/Inertial Navigation System (GPS/INS) navigation model is developed specifically for aerospace applications involving high vehicle dynamics. To aid attitude determination a non-dedicated multiple GPS antenna configuration is employed. Simulated results show that the resulting Extended Kalman Filter (EKF) implementation provides robust estimates of the vehicle states. Additional investigation focusses upon filter performance sensitivity to antenna noise correlation and antenna displacements.","PeriodicalId":359344,"journal":{"name":"Fourth International Symposium on Signal Processing and Its Applications","volume":"53 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Gps/ins Integrated Navigation Using a Gps Antenna Array\",\"authors\":\"K. J. Turner, F. Faruqi\",\"doi\":\"10.1109/ISSPA.1996.615726\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An integrated Global Positioning System/Inertial Navigation System (GPS/INS) navigation model is developed specifically for aerospace applications involving high vehicle dynamics. To aid attitude determination a non-dedicated multiple GPS antenna configuration is employed. Simulated results show that the resulting Extended Kalman Filter (EKF) implementation provides robust estimates of the vehicle states. Additional investigation focusses upon filter performance sensitivity to antenna noise correlation and antenna displacements.\",\"PeriodicalId\":359344,\"journal\":{\"name\":\"Fourth International Symposium on Signal Processing and Its Applications\",\"volume\":\"53 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Fourth International Symposium on Signal Processing and Its Applications\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ISSPA.1996.615726\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Fourth International Symposium on Signal Processing and Its Applications","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISSPA.1996.615726","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Gps/ins Integrated Navigation Using a Gps Antenna Array
An integrated Global Positioning System/Inertial Navigation System (GPS/INS) navigation model is developed specifically for aerospace applications involving high vehicle dynamics. To aid attitude determination a non-dedicated multiple GPS antenna configuration is employed. Simulated results show that the resulting Extended Kalman Filter (EKF) implementation provides robust estimates of the vehicle states. Additional investigation focusses upon filter performance sensitivity to antenna noise correlation and antenna displacements.
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